void applyAndSaveAccelerometerTrimsDelta(rollAndPitchTrims_t *rollAndPitchTrimsDelta)
{
accelerometerConfig()->accelerometerTrims.values.roll += rollAndPitchTrimsDelta->values.roll;
accelerometerConfig()->accelerometerTrims.values.pitch += rollAndPitchTrimsDelta->values.pitch;
saveConfigAndNotify();
}
static void subTaskPidController(timeUs_t currentTimeUs)
{
uint32_t startTime = 0;
if (debugMode == DEBUG_PIDLOOP) {startTime = micros();}
// PID - note this is function pointer set by setPIDController()
pidController(currentPidProfile, &accelerometerConfig()->accelerometerTrims, currentTimeUs);
DEBUG_SET(DEBUG_PIDLOOP, 1, micros() - startTime);
}
static void activateConfig(void)
{
activateControlRateConfig();
resetAdjustmentStates();
useRcControlsConfig(modeActivationProfile()->modeActivationConditions);
pidInitFilters(pidProfile());
#ifdef GPS
gpsUsePIDs(pidProfile());
#endif
useFailsafeConfig();
setAccelerationTrims(&sensorTrims()->accZero);
accelerationFilterInit(accelerometerConfig()->acc_cut_hz);
#ifdef USE_SERVOS
mixerUseConfigs(servoProfile()->servoConf);
#endif
#ifdef GPS
recalculateMagneticDeclination();
#endif
#ifdef VTX
initVTXState();
#endif
static imuRuntimeConfig_t imuRuntimeConfig;
imuRuntimeConfig.dcm_kp = imuConfig()->dcm_kp / 10000.0f;
imuRuntimeConfig.dcm_ki = imuConfig()->dcm_ki / 10000.0f;
imuRuntimeConfig.acc_cut_hz = accelerometerConfig()->acc_cut_hz;
imuRuntimeConfig.acc_unarmedcal = accelerometerConfig()->acc_unarmedcal;
imuRuntimeConfig.small_angle = imuConfig()->small_angle;
imuConfigure(
&imuRuntimeConfig,
&accelerometerConfig()->accDeadband,
accelerometerConfig()->accz_lpf_cutoff,
throttleCorrectionConfig()->throttle_correction_angle
);
}
static FAST_CODE void subTaskPidController(timeUs_t currentTimeUs)
{
uint32_t startTime = 0;
if (debugMode == DEBUG_PIDLOOP) {startTime = micros();}
// PID - note this is function pointer set by setPIDController()
pidController(currentPidProfile, &accelerometerConfig()->accelerometerTrims, currentTimeUs);
DEBUG_SET(DEBUG_PIDLOOP, 1, micros() - startTime);
#ifdef USE_RUNAWAY_TAKEOFF
// Check to see if runaway takeoff detection is active (anti-taz), the pidSum is over the threshold,
// and gyro rate for any axis is above the limit for at least the activate delay period.
// If so, disarm for safety
if (ARMING_FLAG(ARMED)
&& !STATE(FIXED_WING)
&& pidConfig()->runaway_takeoff_prevention
&& !runawayTakeoffCheckDisabled
&& !flipOverAfterCrashMode
&& !runawayTakeoffTemporarilyDisabled
&& (!feature(FEATURE_MOTOR_STOP) || isAirmodeActive() || (calculateThrottleStatus() != THROTTLE_LOW))) {
if (((fabsf(pidData[FD_PITCH].Sum) >= RUNAWAY_TAKEOFF_PIDSUM_THRESHOLD)
|| (fabsf(pidData[FD_ROLL].Sum) >= RUNAWAY_TAKEOFF_PIDSUM_THRESHOLD)
|| (fabsf(pidData[FD_YAW].Sum) >= RUNAWAY_TAKEOFF_PIDSUM_THRESHOLD))
&& ((ABS(gyroAbsRateDps(FD_PITCH)) > RUNAWAY_TAKEOFF_GYRO_LIMIT_RP)
|| (ABS(gyroAbsRateDps(FD_ROLL)) > RUNAWAY_TAKEOFF_GYRO_LIMIT_RP)
|| (ABS(gyroAbsRateDps(FD_YAW)) > RUNAWAY_TAKEOFF_GYRO_LIMIT_YAW))) {
if (runawayTakeoffTriggerUs == 0) {
runawayTakeoffTriggerUs = currentTimeUs + RUNAWAY_TAKEOFF_ACTIVATE_DELAY;
} else if (currentTimeUs > runawayTakeoffTriggerUs) {
setArmingDisabled(ARMING_DISABLED_RUNAWAY_TAKEOFF);
disarm();
}
} else {
runawayTakeoffTriggerUs = 0;
}
DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ENABLED_STATE, DEBUG_RUNAWAY_TAKEOFF_TRUE);
DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ACTIVATING_DELAY, runawayTakeoffTriggerUs == 0 ? DEBUG_RUNAWAY_TAKEOFF_FALSE : DEBUG_RUNAWAY_TAKEOFF_TRUE);
} else {
runawayTakeoffTriggerUs = 0;
DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ENABLED_STATE, DEBUG_RUNAWAY_TAKEOFF_FALSE);
DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ACTIVATING_DELAY, DEBUG_RUNAWAY_TAKEOFF_FALSE);
}
#endif
#ifdef USE_PID_AUDIO
if (isModeActivationConditionPresent(BOXPIDAUDIO)) {
pidAudioUpdate();
}
#endif
}
void subTaskPidController(void)
{
const uint32_t startTime = micros();
// PID - note this is function pointer set by setPIDController()
pidLuxFloat(
pidProfile(),
currentControlRateProfile,
imuConfig()->max_angle_inclination,
&accelerometerConfig()->accelerometerTrims,
rxConfig()
);
if (debugMode == DEBUG_PIDLOOP) {debug[2] = micros() - startTime;}
}
void taskUpdateAccelerometer(void)
{
imuUpdateAccelerometer(&accelerometerConfig()->accelerometerTrims);
}
void taskMainPidLoop(void)
{
cycleTime = getTaskDeltaTime(TASK_SELF);
dT = (float)cycleTime * 0.000001f;
// Calculate average cycle time and average jitter
filteredCycleTime = filterApplyPt1(cycleTime, &filteredCycleTimeState, 1, dT);
debug[0] = cycleTime;
debug[1] = cycleTime - filteredCycleTime;
imuUpdateGyroAndAttitude();
annexCode();
if (rxConfig()->rcSmoothing) {
filterRc();
}
#if defined(BARO) || defined(SONAR)
haveProcessedAnnexCodeOnce = true;
#endif
#ifdef MAG
if (sensors(SENSOR_MAG)) {
updateMagHold();
}
#endif
#if defined(BARO) || defined(SONAR)
if (sensors(SENSOR_BARO) || sensors(SENSOR_SONAR)) {
if (FLIGHT_MODE(BARO_MODE) || FLIGHT_MODE(SONAR_MODE)) {
applyAltHold();
}
}
#endif
// If we're armed, at minimum throttle, and we do arming via the
// sticks, do not process yaw input from the rx. We do this so the
// motors do not spin up while we are trying to arm or disarm.
// Allow yaw control for tricopters if the user wants the servo to move even when unarmed.
if (isUsingSticksForArming() && rcData[THROTTLE] <= rxConfig()->mincheck
#ifndef USE_QUAD_MIXER_ONLY
#ifdef USE_SERVOS
&& !((mixerConfig()->mixerMode == MIXER_TRI || mixerConfig()->mixerMode == MIXER_CUSTOM_TRI) && mixerConfig()->tri_unarmed_servo)
#endif
&& mixerConfig()->mixerMode != MIXER_AIRPLANE
&& mixerConfig()->mixerMode != MIXER_FLYING_WING
#endif
) {
rcCommand[YAW] = 0;
}
if (throttleCorrectionConfig()->throttle_correction_value && (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE))) {
rcCommand[THROTTLE] += calculateThrottleAngleCorrection(throttleCorrectionConfig()->throttle_correction_value);
}
#ifdef GPS
if (sensors(SENSOR_GPS)) {
if ((FLIGHT_MODE(GPS_HOME_MODE) || FLIGHT_MODE(GPS_HOLD_MODE)) && STATE(GPS_FIX_HOME)) {
updateGpsStateForHomeAndHoldMode();
}
}
#endif
// PID - note this is function pointer set by setPIDController()
pid_controller(
pidProfile(),
currentControlRateProfile,
imuConfig()->max_angle_inclination,
&accelerometerConfig()->accelerometerTrims,
rxConfig()
);
mixTable();
#ifdef USE_SERVOS
filterServos();
writeServos();
#endif
if (motorControlEnable) {
writeMotors();
}
#ifdef USE_SDCARD
afatfs_poll();
#endif
#ifdef BLACKBOX
if (!cliMode && feature(FEATURE_BLACKBOX)) {
handleBlackbox();
}
#endif
}
void targetValidateConfiguration(void)
{
if (hardwareRevision < NAZE32_REV5 && accelerometerConfig()->acc_hardware == ACC_ADXL345) {
accelerometerConfigMutable()->acc_hardware = ACC_NONE;
}
}